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Microstructure and tensile properties of BN/SiC coated Hi-Nicalon, and Sylramic SiC fiber preforms
Authors:R. T. Bhatt  Yuan L. Chen  G. N. Morscher
Affiliation:(1) US Army Research Laboratory, National Aeronautics and Space Administration, Glenn Research Center, Cleveland, Ohio 44135, USA;(2) Dynacs Engineering Company, Inc., Brook Park, Ohio 44142, USA;(3) Ohio Aerospace Institute, Brook Park, Ohio 44142, USA
Abstract:Batch to batch and within batch variations, and the influence of fiber architecture on room temperature physical and tensile properties of BN/SiC coated Hi-Nicalon and Sylramic SiC fiber preform specimens were determined. The three fiber architectures studied were plain weave (PW), 5-harness satin (5HS), and 8-harness satin (8HS). Results indicate that the physical properties vary up to 10 percent within a batch, and up to 20 percent between batches of preforms. Load-reload (Hysteresis) and acoustic emission methods were used to analyze damage accumulation occurring during tensile loading. Early acoustic emission activity, before observable hysteretic behavior, indicates that the damage starts with the formation of nonbridged tunnel cracks. These cracks then propagate and intersect the load bearing ldquordquo fibers giving rise to hysteretic behavior. For the Hi-Nicalon preform specimens, the onset of ldquo°rdquo bundle cracking stress and strain appeared to be independent of the fiber architecture. Also, the ldquordquo fiber bundle cracking strain remained nearly the same for the preform specimens of both fiber types. TEM analysis indicates that the CVI BN interface coating is mostly amorphous and contains carbon and oxygen impurities, and the CVI SiC coating is crystalline. No reaction exists between the CVI BN and SiC coating.
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